发明名称 AUTOMATED ASSEMBLY OF PANELIZED AIRCRAFT FUSELAGE
摘要 <P>PROBLEM TO BE SOLVED: To provide a more stable environment for assembling a fuselage of a large civil aircraft. <P>SOLUTION: A facility for assembling the fuselage of an aircraft is provided with two or more movable stands. Each of the stands supports a fuselage keel structure, in which the panelized fuselage is assembled under a single vertical assembled state. More practically, the keel structure is mounted on the stand (a step 510), the assembling columns are fixed to a floor grid, the columns are set down on the panel of the keel structure (a step 520), a lower panel is mounted to a floor beam of the floor grid and assembled (a step 530), an upper panel is mounted (a step 540) and the upper panel can be mounted as an integral structure and further it can also be mounted while being separated. <P>COPYRIGHT: (C)2013,JPO&INPIT
申请公布号 JP2013124099(A) 申请公布日期 2013.06.24
申请号 JP20120271302 申请日期 2012.12.12
申请人 BOEING CO:THE 发明人 OBEROI HARINDER S;NELSON BLAIR P;DRAPER ALAN S;HU CHARLES Y;MATTHEWSON RANDALL;SARH BRANKO
分类号 B64F5/00;B64C1/06 主分类号 B64F5/00
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